GB194114A - Improvements in or relating to metal spars and the like for aviation - Google Patents

Improvements in or relating to metal spars and the like for aviation

Info

Publication number
GB194114A
GB194114A GB4445/22A GB444522A GB194114A GB 194114 A GB194114 A GB 194114A GB 4445/22 A GB4445/22 A GB 4445/22A GB 444522 A GB444522 A GB 444522A GB 194114 A GB194114 A GB 194114A
Authority
GB
United Kingdom
Prior art keywords
corrugation
flange
members
aviation
relating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB4445/22A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB4445/22A priority Critical patent/GB194114A/en
Publication of GB194114A publication Critical patent/GB194114A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Abstract

194,114. Mooney, D. J., and Emby, D. H. Feb. 15, 1922. Addition to 141,141. Framework.-In metal spars &c. for aircraft, wherein channel section web members having an outwardly turned corrugation adjacent to each. flange have their flanges riveted to flange members each having a deep central longitudinal corrugation and two inwardly turned side corrugations forming abutments for the channel members, as described in the parent Specification, the flange members are so shaped that the riveted joints are nearer to the neutral axis than the parts f, g of the flange members. The form shown has an additional inwardly turned corrugation h formed in the deepcentral corrugation a of each flange member.
GB4445/22A 1922-02-15 1922-02-15 Improvements in or relating to metal spars and the like for aviation Expired GB194114A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4445/22A GB194114A (en) 1922-02-15 1922-02-15 Improvements in or relating to metal spars and the like for aviation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4445/22A GB194114A (en) 1922-02-15 1922-02-15 Improvements in or relating to metal spars and the like for aviation

Publications (1)

Publication Number Publication Date
GB194114A true GB194114A (en) 1923-03-08

Family

ID=9777302

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4445/22A Expired GB194114A (en) 1922-02-15 1922-02-15 Improvements in or relating to metal spars and the like for aviation

Country Status (1)

Country Link
GB (1) GB194114A (en)

Similar Documents

Publication Publication Date Title
GB125748A (en) Improvements in Construction of Metal Spars and Longerons for Aircraft.
GB194114A (en) Improvements in or relating to metal spars and the like for aviation
GB134276A (en) Improvements in Rolls for Forming Metal Parts for Aviation.
GB218074A (en) Improvements in or relating to metal spars and the like for aircraft
GB128846A (en) Improvements in Metal Construction for Aircraft.
GB220383A (en) Improvements in metal framework for aircraft
GB157312A (en) Improvement in airplane spars
GB263264A (en) Improvements in the construction of framework members for aircraft
GB193088A (en) Improved construction of joint for frames of hollow metal structures
GB253960A (en) Improvements in or relating to metal spars and the like for aircraft
GB180074A (en) Improvements in metal framework for aircraft
GB121006A (en) Improvements in Metal Spars for Aircraft.
USD85639S (en) Panies
GB202761A (en) Improvements in or relating to spars for aircraft
GB150783A (en) Improvements in metal members for aircraft
GB289599A (en) Improvements in or relating to expansion joints for piping
GB223670A (en) Improvements in or relating to metal spars and the like for aviation
GB141141A (en) Improvements in or relating to metal spars and the like for aviation
GB330514A (en) Improvements in mouldings for vehicle bodies and other structures
GB465246A (en) Improvements relating to metal aeroplane bodies
GB247313A (en) Improvements in the construction of aircraft members
GB131080A (en) Improvements in the Construction of Metal Spars for Aircraft.
GB211606A (en) Improvements in the construction of structural members for aircraft
GB361010A (en) Improvements in and relating to metal spars and the like for aircraft
GB214847A (en) Improvements in or relating to the construction of spars for aircraft